US4487064A - Internal gate rotary vane fluid meter with controlled rotor vane inner diameter - Google Patents

Internal gate rotary vane fluid meter with controlled rotor vane inner diameter Download PDF

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US4487064A
US4487064A US06/494,206 US49420683A US4487064A US 4487064 A US4487064 A US 4487064A US 49420683 A US49420683 A US 49420683A US 4487064 A US4487064 A US 4487064A
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United States
Prior art keywords
gate
rotor
vane
vanes
fluid
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Expired - Fee Related
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US06/494,206
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English (en)
Inventor
Irwin A. Hicks
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AMERICA METER Co
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Singer Co
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Priority to US06/494,206 priority Critical patent/US4487064A/en
Assigned to SINGER COMPANY, THE reassignment SINGER COMPANY, THE ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: HICKS, IRWIN A.
Priority to CA000450318A priority patent/CA1201306A/en
Priority to AU27652/84A priority patent/AU564407B2/en
Priority to JP59093821A priority patent/JPS59212717A/ja
Priority to DE198484105380T priority patent/DE125664T1/de
Priority to BR8402288A priority patent/BR8402288A/pt
Priority to EP84105380A priority patent/EP0125664B1/en
Priority to DE8484105380T priority patent/DE3467404D1/de
Priority to DK236184A priority patent/DK236184A/da
Priority to KR1019840002563A priority patent/KR850000062A/ko
Publication of US4487064A publication Critical patent/US4487064A/en
Application granted granted Critical
Assigned to AMERICA METER COMPANY reassignment AMERICA METER COMPANY ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: SINGER COMPANY THE, A CORP. OF NEW JERSEY
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M31/00—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F3/00—Measuring the volume flow of fluids or fluent solid material wherein the fluid passes through the meter in successive and more or less isolated quantities, the meter being driven by the flow
    • G01F3/02—Measuring the volume flow of fluids or fluent solid material wherein the fluid passes through the meter in successive and more or less isolated quantities, the meter being driven by the flow with measuring chambers which expand or contract during measurement
    • G01F3/04—Measuring the volume flow of fluids or fluent solid material wherein the fluid passes through the meter in successive and more or less isolated quantities, the meter being driven by the flow with measuring chambers which expand or contract during measurement having rigid movable walls
    • G01F3/06—Measuring the volume flow of fluids or fluent solid material wherein the fluid passes through the meter in successive and more or less isolated quantities, the meter being driven by the flow with measuring chambers which expand or contract during measurement having rigid movable walls comprising members rotating in a fluid-tight or substantially fluid-tight manner in a housing

Definitions

  • This invention relates to fluid meters and, more particularly, to a fluid meter of the internal gate rotary vane type.
  • Rotary vane-type fluid meters with an internal sealing gate generally exhibit excellent performance characteristics compared to other types of rotary positive displacement meters (such as the lobed impeller or external sealing gate type meters). As a general rule, the reason for better performance is better fluid flow through the meter and lower friction of the moving parts.
  • Fluid meters have exacting requirements for minimum performance. For a given full capacity rating, a meter must not exceed some standard of maximum pressure drop, or differential, across the meter connections (as this is a measure of its lack of friction and flow impediments). For gaseous rotary meters this standard is presently one inch water column (1/27 psig) at full capacity on natural gas (0.6 S.G.) where the inlet is at seven inches water column (1/4 psig) over atmospheric pressure. As some pressure differential would normally occur across a pipe of equal length, connection to connection, such a requirement dictates low friction of mechanism and minimal fluid flow impediments. It follows that designs having lower mechanical friction and fewer flow impediments have a higher capacity and thus more commercial value.
  • Another measure of fluid meter performance is accuracy of measuring actual volume from low flow rates to capacity. While 100% accuracy is desirable at all flow rates, it is recognized as being impossible. Accordingly, industry standards use a minimum level of performance which allow some deviations in accuracy. In the United States for gaseous rotary meters this standard presently is a band of ⁇ 1% around 100% accuracy for flow rates which the meter must meet during many years of operation without calibration, at all rated pressures, and in all conceivable ambient temperatures. Therefore, a meter with minimal friction and fewer flow impediments is more likely to meet accuracy requirements given such operating conditions.
  • Rangeability is defined, for gaseous meters, as the ratio of full flow rate divided by that lower flow rate which falls out of the accuracy band of 100% ⁇ 1%. Rangeability is expressed as a ratio (such as 20:1 which would mean the meter's accuracy was falling below 99% at 5% of full flow). This performance criteria is a very sensitive measure of the meter's mechanical friction and/or freedom from compression/suction cycles as these cause the rotating components to try to operate slower than the gas velocity, which results in blowby at the seals. Rangeability can also be a measure of the sealing effectiveness (seal blowby at a given differential), but mechanical friction and/or compression/suction cycles cause the increased pressure differential to drive fluids through the seal.
  • FIG. 1 illustrates a typical performance chart for a gaseous rotary meter.
  • the highest accuracy values cannot exceed 101% (see Points B and C) and the lowest accuracy values cannot be lower than 99%, including compression frequencies (see Point D) and "boost” or “droop” at full capacity (Point E is a "droop", F is a "boost”).
  • the Rangeability of this example is 20:1 (or 100% ⁇ 5%, the point at which the accuracy curve falls below 99%, Point G).
  • the flange-to-flange pressure differential cannot exceed 1.0" H 2 O (see Point H) for 7.0" H 2 O inlet pressure.
  • a rotary meter having a high operating pressure differential due to mechanical friction or flow impediments would result in the capacity being lowered until the 1.0" H 2 O differential were met.
  • a rotary meter with substantial compressive cycles might not even qualify to the standard.
  • a rotary meter with high rotational velocity friction due to such items as geared gate driving mechanisms, bearings, lubricating baths, and seals, or flow rate related impediments, might have excessive "droop" as to limit capacity.
  • a rotary meter whose accuracy is adversely affected by pressure might not qualify.
  • a rotary meter having high tare friction (and possibly poor sealing) might substantially reduce rangeability.
  • a fluid meter having a gate with at least two pockets which rotates at the same velocity as a rotor having the same number of vanes and wherein the inner diameter of the rotor vanes is controlled to provide a properly sized orifice between the vane inner diameter surface and the gate hub so as to provide a driving torque to the gate due to the passage of the vanes through the gate pocket, the gate driving torque being balanced to match gate retarding torques due to friction of the gate drive train and friction of the gate bearings.
  • FIG. 1 illustrates a typical performance chart for a rotary gaseous meter
  • FIGS. 2A-2F are schematic cross sectional views useful in understanding the principles of operation of an internal gate rotary vane fluid meter
  • FIGS. 3, 4 and 5 illustrate the passage of a vane through a pocket from the perspective of a pocket which is stationary relative to the viewer;
  • FIG. 6 illustrates the compression/suction forces acting on the gate due to passage of a vane through a pocket
  • FIG. 7 illustrates the travel of a vane through a pocket for a 3 pocket/4 vane configuration
  • FIG. 8 illustrates the travel of a vane through a pocket for a 3 pocket/3 vane configuration
  • FIG. 9 illustrates the volume swept by a vane in one revolution
  • FIG. 10 illustrates the dimensions of the configuration shown in FIGS. 2A-2F;
  • FIG. 11 illustrates a modification to FIG. 10
  • FIG. 12 illustrates a further modification to FIG. 10
  • FIGS. 13A and 13B illustrate 3 and 4 vane rotors, respectively, with equal numbers of pockets, in which the swept volume is maximized;
  • FIGS. 14A and 14B illustrate, respectively, a double ended rotor and a cantilevered vane rotor
  • FIGS. 15A and 15B illustrate the area differences between inlet/outlet piping and vanes for the constructions of FIGS. 14A and 14B, respectively;
  • FIG. 16 illustrates the flow through a 3 vane/3 pocket meter
  • FIG. 17 shows a typical connection to a pipe run of the meter shown in FIG. 16.
  • FIG. 18 schematically shows the flow through the meter of FIG. 17
  • FIGS. 19A and 19B schematically show the flow through the meters of FIGS. 13A and 13B, respectively.
  • FIG. 20 illustrates a preferred housing and gate/rotor configuration.
  • FIGS. 2A-2F are section views of a contemporary meter showing rotor 10, rotor vanes 11, 12, 13 and 14, gate 30, gate pockets 31 and 32, housing 50, inlet port 51, outlet port 52, and sealing crescent 53.
  • Such construction can be observed in Wrinkle's U.S. Pat. No. 3,482,446 as improved by Schneider's U.S. Pat. No. 4,109,528 and Schneider's U.S. Pat. No. 3,554,032 as improved by Schneider's U.S. Pat. No. 3,842,672.
  • These patents cover the only known commercially available vane-type rotary meters with an internal seal gate.
  • FIG. 2A it can be observed that incoming fluid can fill the inlet cavity 54 until stopped by the seal gate 30 and vane 12.
  • the seals on gate 30 are effected against the housing 50 at the gate cavity 55 at the point 33 and against the sealing crescent 53 at the point 34.
  • These seal points 33 and 34 must be sufficiently tight (small clearance) and long enough to substantially impede fluid flow when the outlet port 52 is at a lower pressure than the inlet port 51.
  • the seals on the rotor vane 12 are effected at the housing 50 at the rotor 10 outer diameter at point 15 and at the inner diameter at point 16 against the crescent 53. Again the seal points 15 and 16 must be sufficiently tight and long enough to substantially impede fluid flow.
  • the gate 30 is also driven counterclockwise (generally by timing gearing) so as to synchronize the gate pocket 31 with the passage of the leaving vane 11 and the gate pocket 32 with the returning vane 14.
  • timing gearing generally by timing gearing
  • FIG. 2C a portion of fluid has now been trapped between vanes 11 and 12 which, for these illustrations, becomes the measured actual volume.
  • the measured volume also includes the gate pocket 31 volume less the returning gate pocket 32 volume, the latter being smaller because of the vane 14 displacement which makes up for half each of vanes 11 and 12 displacement. This is why the capacity of the meter is the swept area of the vanes and ignores the vane thickness.
  • FIGS. 2D-2F continue the cycle until, in FIG. 2F, the measured gas is expelled to the outlet port 52.
  • FIGS. 2A-2F show a 2 pocket gate and 4 vane rotor with relative rotational velocities in the ratio of 2 to 4; i.e., the gate 30 rotational velocity is twice (200%) that of the rotor 10. It is well known that any other ratio which synchronizes the vanes into gate pockets will work (but is not necessarily preferred) as long as there are at least two vanes (required for sealing).
  • FIG. 3 allows the viewer to maintain a constant perspective of a gate pocket while observing the passage of a rotor vane with respect to rotational position.
  • the example shown is the FIGS. 2A-2F example of 2 gate pocket/4 rotor vane configuration with the gate rotational velocity being twice the rotor rotational velocity. It would appear, from examination of FIG. 3, that fluid turbulence is relatively minimal in the pocket (especially compared to lobed or external gate designs), and indeed it is. However, further examination reveals that there are some compression/suction cycles even with a good basic entry and exit of the vane in a gate pocket.
  • FIG. 3 allows the viewer to maintain a constant perspective of a gate pocket while observing the passage of a rotor vane with respect to rotational position.
  • the example shown is the FIGS. 2A-2F example of 2 gate pocket/4 rotor vane configuration with the gate rotational velocity being twice the rotor rotational velocity. It would appear, from examination of FIG. 3, that fluid turbulence is relatively minimal in
  • FIG. 3 shows the FIG. 2B position of FIG. 3 crosshatched with an area of fluid 36 dotted.
  • FIG. 5 shows the FIG. 2C position of FIG. 3 cross-hatched with the same area of fluid 36 dotted.
  • the vane 14 (at FIG. 2C crosshatched) has now completely entered the pocket 32.
  • the entry of the vane 14 displaced some fluid (that area of the vane under the line 40) and it can be presumed that half of the displaced fluid went to either side of the vane 14.
  • That portion of the fluid displaced by the vane 14 pertinent to the discussion is 41 (it causes a compression to area 36).
  • the vane 14 has vacated an area 42 (shown as joined circles) which is a suction to area 36.
  • Area 42 (the suction) is larger than area 41 (the compression) so the net effect is a suction on area 36.
  • the rotor 10 is the driving force in a meter (due to pressure differential from inlet to outlet).
  • the rotor 10 through some driving mechanism (like gears) causes the gate 30 to be driven. While the drive to the gate 30 is a modest torque, it should be noted that it is through a 200% speed increaser (for a 2 pocket gate, 4 vane rotor); which more than doubles the required torque from the rotor 10 to drive the gate 30. It is more than double the torque because gear train and bearing friction increase with rotational velocity.
  • FIG. 6 shows a diagram of resultant forces. It can be seen in FIG.
  • Such a 2 pocket/4 vane rotor arrangement can also be observed to have, of the possible available combinations of gate/rotor ratios, the one of the higher gate rotational velocities which results in higher gate drive train frictions, higher gate bearing rotational velocities and resultant friction (which also lowers bearing life), and has higher rotating element inertia (if the mass and diameters of components are identical).
  • FIG. 7 uses the technique of FIGS. 3-5 to show the characteristics of vane entry/exit to a gate pocket. It can be observed in FIG. 7 that the vane entry/exit is not like the FIG. 3 example. In FIG. 7, the vane 21 has a higher angle of attack to the gate pocket 22.
  • an additional benefit of this 1:1 ratio is that other types of gate driving mechanism (than gear trains) are possible.
  • Another benefit is that the inertia of rotating elements is minimized (for rotating elements of the same diameter and mass). Reduction in rotating component inertia allows the meter to be more responsive to changes in fluid flow rate, improves measured accuracy during a change in flow rate (lower inertia reduces the pressure differential across the rotating elements which reduces seal blowby), reduces mechanical strain on components due to sudden, major changes in flow rate, reduces the mechanical strain on the gate drive train, and reduces the overrun/reverse characteristics of rotary meters which occurs when the flow rate is quickly reduced (such as the reduction of a burner to a pilot flame) which can extinguish ("suck-out") a pilot.
  • Another benefit is that bearing velocity of the gate components is reduced so that bearing life is improved.
  • the preferred embodiment should have a 1:1 gate to rotor rotational velocity ratio of at least 2 gate pockets/2 rotor vanes where the aiding forces of the vane passage through the gate pocket is balanced (by trimming the vane inner diameter to provide the desired orifice 26) against the forces of the gate drive friction and gate bearing friction.
  • Proper dimensions of the orifice 26 are obtained through empirical testing, since different sized meters have different bearings, etc., which results in different retarding forces. Additional benefits of this lowest practical ratio are lowest gate drive friction, lowest gate bearing friction, and lowest inertia of rotating components (for a given diameter and mass of rotating components). The effect on meter performance is to improve and stabilize accuracy over wide flow rates and to reduce pressure differential (which improves capacity) and to improve rangeability.
  • rotor, gate, and crescent geometry Another consideration is rotor, gate, and crescent geometry.
  • rotational velocity friction By minimizing rotational velocity friction, inaccuracies due to variable friction are minimized and rangeability is improved (increase in ratio).
  • the objective in selecting geometry is therefore to minimize component rotational velocity.
  • the capacity per revolution of a rotary vane meter is the swept area of a rotor vane in one revolution.
  • the vane 46 outer diameter is D r
  • the vane 46 inner diameter is D i
  • the vane 46 length is L v
  • the swept volume (or capacity) V in one revolution is a cylinder having a volume as follows:
  • D i has some constraints to reducing its diameter.
  • one major constraint is that the gate bearing hub diameter D h must be inside the vane inner diameter D i so that the vane 11 can pass the gate 30.
  • Another major constraint is that the gate hub must have a vane inner tip orifice 38 for balancing vane driving torque to friction (as previously discussed).
  • FIG. 9 capacity per revolution
  • D r and vane length L v in FIG. 9
  • FIGS. 11 and 12 demonstrate the effect of D i if the gate diameter D g is maximized (within its constraints).
  • FIG. 13A shows a 3 vane rotor and FIG. 13B shows a 4 vane rotor which have an increased gate diameter D g which still seals appropriately. It can be observed in FIGS. 13A and 13B that for the identical rotor diameter D r in FIGS. 10-12, increasing the gate diameter D g to the maximum (which still affords sealing) by reducing the crescent to its minimum sealing requirement reduces the rotor vane inner diameter D i to its minimum value. This, in turn, maximizes the volume V for a given rotor outer diameter D r and vane length L v .
  • This reduction in friction improves meter performance; variances in accuracy due to friction are reduced, pressure differential to drive the rotor is reduced (thus capacity rating is increased), and rangeability can be improved both due to lower rotating friction as well as lower driving pressure differential.
  • the rotating inertia is reduced in proportion to rotating velocity for the rotor, and to a lesser degree for the gate (as it is a larger diameter). This improves meter response during changes in flow rate.
  • W v width of the vane at its inner circumference
  • rotor vane length (L v in FIG. 9). It has been the practice in rotary meter design to maximize the length of vanes (length parallel) to the axis of rotor rotation) within the constraints of mechanical construction. For instance, contemporary 4 vaned rotors with a rotor end plate on both ends have a vane length L v to rotor diameter D r ratio of 1:1. Contemporary 3 vaned rotors with cantilevered vanes from one rotor end plate have a vane length L v to rotor diameter D r ratio of 1:2. These constructions are illustrated in FIGS. 14A and 14B, respectively.
  • FIGS. 15A and 15B graphically illustrates this aspect ratio issue.
  • Such fluid dynamic effects are proportional to fluid mass; thus the adverse effects of a higher aspect ratio is more pronounced at higher (i.e., capacity) flow rates and when the fluid's mass increases (i.e., at higher pressures for gaseous fluids).
  • another reason to limit the aspect ratio is to minimize effects of gas density.
  • Another effect of limiting the aspect ratio is that increasing the rotor diameter to compensate for reduced vane length results in improved volumetric efficiency (the ratio of the swept volume to the volume occupied by the mechanism), because as shown in FIG. 9, the swept volume is related to the second power of the diameter (D 2 ) but only to the first power of the vane length (L v ); this allows a lower rotational velocity of the rotor. As previously observed, slowing component rotational velocity reduces rotating friction proportionately. It should be noted, however, that rotational inertia is reduced in proportion to the lower rotational velocity but increased due to the outward movement of rotating component mass (rotating component design must attempt to minimize mass towards the component periphery).
  • Another effect of limiting the aspect ratio by increasing the rotor diameter and shortening rotor vanes is that the starting torque is increased in proportion to the increase in diameter of the rotor (the force, pressure differential, of liquid against the rotor vane has a larger moment arm around the rotor centerline).
  • This increase in starting torque is highly beneficial to rangeability as the rotating components more readily overcome tare friction of gate drive and bearings allowing the rotor to more nearly match the velocity of the measured fluid at low flow rates (which are also at very low pressure differentials).
  • This additional torque is also very beneficial in driving devices powered by a rotor (such as mechanical volume correctors).
  • FIG. 17 shows a typical method.
  • the problem with the method shown in FIG. 17, however, is that fluids tend (due to their mass) to continue in the same direction and velocity as their initial direction and velocity in the entrance pipe or as exiting the meter outlet chamber 75.
  • pressure differential is one of the parameters of meter rating.
  • FIG. 18 shows this schematically. In the schematic FIG. 18, (and referring to FIG.
  • FIGS. 13A and 13B disclose this principle.
  • the amount of fluid turning can be substantially reduced depending on the number of vanes on the rotor; from 360° arc to 240° arc for a 3 vane rotor (FIG. 19A), and from 360° arc to 180° arc for a 4 vane rotor (FIG. 19B).
  • the radius R 1 for the inlet conduits 79, 81 and the radius R 2 for the outlet conduits 80, 82 can be made larger (more gentle turn) without significantly increasing the flange-to-flange dimension W f .
  • the result of this approach is to significantly lower the differential pressure required to pass fluid through the housing (without rotating elements). Benefits are higher capacity rating for a given pipe size and reduction in gaseous fluid density effects as might occur with higher pressures.
  • the preferred embodiment is a 3 vane rotor (due to the geometry of rotating elements in a 1:1 ratio of gate to rotor rotational velocities with a maximized gate diameter and balanced torque orifice as herein described).
  • the suction and compression points next to the gate are significantly detached from the fluid flow as shown in FIGS. 19A and 19B but absolutely require fluid flow.
  • the tapered fluid inlet and outlet chambers are required for proper fluid feed and exit to gate and rotor.
  • a "practical" meter housing 83 which minimizes pressure differential losses due to fluid dynamic considerations of turning and changes in velocity.
  • the rotor 100 and gate 101 are mounted on the housing 83 for rotation about parallel displaced axes. If the inlet pipe fluid flow and cross-sectional area is considered to be 100%, then chamber 84 also is 100% (but can be used to convert from the circular pipe inner diameter to rectangular shape as a transition). Turning vane 85 splits the 100% into the fluid flow requirement behind the turning vanes at the rotor (the tapered inlet chamber 73 of FIG.
  • the result to performance is improved accuracy (particularly at full capacity) and reduced aberrations of accuracy due to gaseous fluid density (as at higher operating pressures).
  • a housing configuration for in-line piping of conduits and turning vanes structured to fulfill the fluid feeding requirements at the rotor while directing most of the fluid flow through gently curving conduits which reduce the typical 360° arc of fluid flow through the meter to 240° of arc thus improving accuracy at high flow rates and/or at higher operating pressures.
  • the reduced crescent (under 180° of arc) is a prerequisite to this design.
  • a body configured with passages whose total cross-sectional area on the inlet or outlet side substantially equals the area of the vane (length times depth).

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Measuring Volume Flow (AREA)
  • Rotary Pumps (AREA)
US06/494,206 1983-05-13 1983-05-13 Internal gate rotary vane fluid meter with controlled rotor vane inner diameter Expired - Fee Related US4487064A (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
US06/494,206 US4487064A (en) 1983-05-13 1983-05-13 Internal gate rotary vane fluid meter with controlled rotor vane inner diameter
CA000450318A CA1201306A (en) 1983-05-13 1984-03-23 Internal gate rotary vane fluid meter with controlled rotor vane inner diameter
AU27652/84A AU564407B2 (en) 1983-05-13 1984-05-03 Internal gate rotary vane fluid meter
JP59093821A JPS59212717A (ja) 1983-05-13 1984-05-10 制御されたロ−タ−ベ−ン内径を有する内部ゲ−トロ−タリ−ベ−ン流量計
EP84105380A EP0125664B1 (en) 1983-05-13 1984-05-11 Internal gate rotary vane fluid meter with controlled rotor vane inner diameter
BR8402288A BR8402288A (pt) 1983-05-13 1984-05-11 Medidor de fluido com comporta de alhetas rotativas,com diametro interno das alhetas de rotor controlado
DE198484105380T DE125664T1 (de) 1983-05-13 1984-05-11 Drehkolbenfluessigkeitszaehler mit innenliegendem drehschieber und kontrolliertem innendurchmesser der drehkolbenfluegel.
DE8484105380T DE3467404D1 (de) 1983-05-13 1984-05-11 Internal gate rotary vane fluid meter with controlled rotor vane inner diameter
DK236184A DK236184A (da) 1983-05-13 1984-05-11 Fluidummaaler med indvendig roterende port og skovlblade og dimensionering af skovlbladets indvendige diameter
KR1019840002563A KR850000062A (ko) 1983-05-13 1984-05-12 제어된 회전자 날개 내경을 구비한 내부 게이트 회전익 유량계

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Application Number Priority Date Filing Date Title
US06/494,206 US4487064A (en) 1983-05-13 1983-05-13 Internal gate rotary vane fluid meter with controlled rotor vane inner diameter

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US4487064A true US4487064A (en) 1984-12-11

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US06/494,206 Expired - Fee Related US4487064A (en) 1983-05-13 1983-05-13 Internal gate rotary vane fluid meter with controlled rotor vane inner diameter

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US (1) US4487064A (da)
EP (1) EP0125664B1 (da)
JP (1) JPS59212717A (da)
KR (1) KR850000062A (da)
AU (1) AU564407B2 (da)
BR (1) BR8402288A (da)
CA (1) CA1201306A (da)
DE (2) DE125664T1 (da)
DK (1) DK236184A (da)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5513529A (en) * 1991-06-07 1996-05-07 Liquid Controls Corporation Housing assembly for flow meter
DE202017106254U1 (de) * 2017-10-16 2019-01-17 Flaco-Geräte GmbH Durchflussmessgerät
CN110645237A (zh) * 2019-09-02 2020-01-03 厦门理工学院 一种管道导流装置

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1994397A (en) * 1933-03-23 1935-03-12 Loveridge Claude Warren Rotary engine
US3482446A (en) * 1966-04-25 1969-12-09 American Meter Co Fluid meter
US3950990A (en) * 1973-10-03 1976-04-20 Dresser Europe, S.A. Bulk flow meter
US4253333A (en) * 1979-09-24 1981-03-03 The Singer Company Rotary meter

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3842672A (en) * 1973-05-09 1974-10-22 Singer Co Flow profiler for high pressure rotary meters

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1994397A (en) * 1933-03-23 1935-03-12 Loveridge Claude Warren Rotary engine
US3482446A (en) * 1966-04-25 1969-12-09 American Meter Co Fluid meter
US3950990A (en) * 1973-10-03 1976-04-20 Dresser Europe, S.A. Bulk flow meter
US4253333A (en) * 1979-09-24 1981-03-03 The Singer Company Rotary meter

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5513529A (en) * 1991-06-07 1996-05-07 Liquid Controls Corporation Housing assembly for flow meter
DE202017106254U1 (de) * 2017-10-16 2019-01-17 Flaco-Geräte GmbH Durchflussmessgerät
CN110645237A (zh) * 2019-09-02 2020-01-03 厦门理工学院 一种管道导流装置
CN110645237B (zh) * 2019-09-02 2022-01-14 厦门理工学院 一种管道导流装置

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BR8402288A (pt) 1984-12-18
DK236184A (da) 1984-11-14
AU2765284A (en) 1984-11-15
EP0125664A1 (en) 1984-11-21
DE125664T1 (de) 1985-02-14
DE3467404D1 (de) 1987-12-17
EP0125664B1 (en) 1987-11-11
DK236184D0 (da) 1984-05-11
KR850000062A (ko) 1985-02-25
CA1201306A (en) 1986-03-04
JPS59212717A (ja) 1984-12-01
AU564407B2 (en) 1987-08-13

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